Distributed Attitude Consensus of Multiple Flexible Spacecraft, Chen

Автор: You Rui, Gao Wenjun, Wu Chunbang
Название: Technologies for Spacecraft Antenna Engineering Design
ISBN: 9811558329 ISBN-13(EAN): 9789811558320
Издательство: Springer
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Цена: 167700.00 T
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Описание: Overview.- Spacecraft TT&C Antenna.- Spacecraft DTA.- Spacecraft GNSS Antenna.- Intersatellite Link Antenna.- Communication Satellite Payload Antenna.- Microwave Remote Sensing Satellite Payload Antenna.- Low Frequency Antenna and Small Satellite Antenna.- Reliability Design of Spacecraft Antenn.- Spacecraft Antenna Test Technology.- Design Case of Typical Spacecraft Antenna System.- Overview of New Technology of Spacecraft Antenna.

Автор: F. Landis Markley; John L. Crassidis
Название: Fundamentals of Spacecraft Attitude Determination and Control
ISBN: 1493955691 ISBN-13(EAN): 9781493955695
Издательство: Springer
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Цена: 69650.00 T
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Описание: It provides detailed derivations for attitude kinematics and dynamics and provides detailed description of the most widely used attitude parameterization, the quaternion.

Автор: J. Jaap Wijker
Название: Random Vibrations in Spacecraft Structures Design
ISBN: 9400736797 ISBN-13(EAN): 9789400736795
Издательство: Springer
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Цена: 130590.00 T
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Описание: This book examines low and high frequency mechanical, acoustic random vibrations. The theory of random vibration is strongly related to the design of spacecraft structures and is illustrated with simple and more difficult worked examples.

Автор: Chen
Название: Distributed Attitude Consensus of Multiple Flexible Spacecraft
ISBN: 9811942579 ISBN-13(EAN): 9789811942570
Издательство: Springer
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Цена: 93160.00 T
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Описание: This book mainly presents the authors' recent studies on the distributed attitude consensus of multiple flexible spacecraft. Modified Rodrigues parameters and rotation matrix are used to represent spacecraft attitude. Several distributed adaptive controllers are presented with theoretical analyses, numerical simulations and experimental verifications. The authors intend to provide a manual that allows researchers, engineers and students in the field of aerospace engineering and mechanics to learn a theoretical and practical approach to the design of attitude consensus algorithms.

Автор: Hu Qinglei, Li Bo, Xiao Bing
Название: Control Allocation for Spacecraft Under Actuator Faults
ISBN: 981160438X ISBN-13(EAN): 9789811604386
Издательство: Springer
Цена: 130430.00 T
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Описание: This book provides a systematical and comprehensive description of some facets of modeling, designing, analyzing and exploring the control allocation and fault-tolerant control problems for over-actuated spacecraft attitude control system under actuator failures, system uncertainties and disturbances.

Автор: F. Landis Markley; John L. Crassidis
Название: Fundamentals of Spacecraft Attitude Determination and Control
ISBN: 1493908014 ISBN-13(EAN): 9781493908011
Издательство: Springer
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Цена: 83850.00 T
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Описание: It provides detailed derivations for attitude kinematics and dynamics and provides detailed description of the most widely used attitude parameterization, the quaternion.

Автор: Hu, Qinglei
Название: Fault Tolerant Attitude Control Of Spacecraft
ISBN: 0323898637 ISBN-13(EAN): 9780323898638
Издательство: Elsevier Science
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Цена: 151590.00 T
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Описание:

Fault-Tolerant Attitude Control of Spacecraft presents the fundamentals of spacecraft fault-tolerant attitude control systems, along with the most recent research and advanced, nonlinear control techniques. This book gives researchers a self-contained guide to the complex tasks of envisaging, designing, implementing and experimenting by presenting designs for integrated modeling, dynamics, fault-tolerant attitude control, and fault reconstruction for spacecraft. Specifically, the book gives a full literature review and presents preliminaries and mathematical models, robust fault-tolerant attitude control, fault-tolerant attitude control with actuator saturation, velocity-free fault tolerant attitude control, finite-time fault-tolerant attitude tracking control, and active fault-tolerant attitude contour.

Автор: Wang Jie, Li Dong-Xu
Название: Rigid-Flexible Coupling Dynamics and Control of Flexible Spacecraft with Time-Varying Parameters
ISBN: 9811650969 ISBN-13(EAN): 9789811650963
Издательство: Springer
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Цена: 121110.00 T
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Описание: This book presents the dynamic modeling and attitude control of flexible spacecraft with time-varying parameters.

Автор: Leonardo Mazzini
Название: Flexible Spacecraft Dynamics, Control and Guidance
ISBN: 331925538X ISBN-13(EAN): 9783319255385
Издательство: Springer
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Цена: 139310.00 T
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Описание: This book is an up-to-date compendium on spacecraft attitude and orbit control (AOC) that offers a systematic and complete treatment of the subject with the aim of imparting the theoretical and practical knowledge that is required by designers, engineers, and researchers.

Автор: Wang
Название: Rigid-Flexible Coupling Dynamics and Control of Flexible Spacecraft with Time-Varying Parameters
ISBN: 9811650993 ISBN-13(EAN): 9789811650994
Издательство: Springer
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Цена: 121110.00 T
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Описание: This book presents the dynamic modeling and attitude control of flexible spacecraft with time-varying parameters. The dynamic characteristics, vibration control methods and attitude stabilization methods for spacecraft are systematically studied in respects of the theoretical modeling, numerical simulation and the ground experiment. Three active control theories in complex mode space are presented for flexible space structures. Optimal slew strategies based on variable amplitudes input shaping methods and coupling control methods are proposed for stabilization of flexible spacecraft. The research provides an important way to solve the problem of high-precision attitude control of flexible spacecraft with time-varying parameters. This book is appropriate for the researchers who focus on the multi-body dynamics, attitude and vibration control of flexible spacecraft.

Автор: Yang, Yaguang
Название: Spacecraft Modeling, Attitude Determination, and Control
ISBN: 0367780356 ISBN-13(EAN): 9780367780357
Издательство: Taylor&Francis
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Цена: 53070.00 T
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Автор: Hu
Название: Intelligent Autonomous Control of Spacecraft with Multiple Constraints
ISBN: 9819906806 ISBN-13(EAN): 9789819906802
Издательство: Springer
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Цена: 149060.00 T
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Описание: This book explores the intelligent autonomous control problems for spacecraft with multiple constraints, such as pointing/path constraints, linear/angular velocity constraints, performance constraints, etc. It provides an almost self-contained presentation of dynamics modeling, controller design and analysis, as well as simulation studies. The book aims to offer a valuable guide for researchers and aerospace engineers to address the theoretical and technical difficulties in different applications, ranging from spacecraft attitude reorientation and tracking to spacecraft proximity operations, and is mainly intended for technical and engineering staff engaged in spacecraft dyanmics and control areas.